Motor control architecture for simultaneously controlling multiple motors

Abstract

A motor control architecture is provided that simultaneously controls multiple motors. The motor control system includes memory, a plurality of motor control processors, and a communication controller. The motor control processors are each responsive to control signals supplied from the communication controller to selectively retrieve system commands and motor positions from the memory, to generate motor commands, and to supply the generated motor commands to the memory. The communication controller selectively receives system commands and transmits the received system commands to the memory, selectively supplies the command signals to selected ones of the motor control processors, selectively receives motor positions from a plurality of motors, selectively transmits motor positions to the memory, selectively retrieves generated motor commands supplied to the memory, and selectively transmits the retrieved motor commands.

Description

TECHNICAL FIELD[0001]The present invention generally relates to motor controls and, more particularly, to a motor control architecture that allows for a single device to simultaneously control multiple motors.BACKGROUND[0002]Aircraft typically include a plurality of flight control surfaces that, when controllably positioned, guide the movement of the aircraft from one destination to another. The number and type of flight control surfaces included in an aircraft may vary, but typically include both primary flight control surfaces and secondary flight control surfaces. The primary flight control surfaces are those that are used to control aircraft movement in the pitch, yaw, and roll axes, and the secondary flight control surfaces are those that are used to influence the lift or drag (or both) of the aircraft. Although some aircraft may include additional control surfaces, the primary flight control surfaces typically include a pair of elevators, a rudder, and a pair of ailerons, and ...

AI Technical Summary

Problems solved by technology

Though unlikely, it is postulated that a flight control surface actuator could become inoperable.

However, these systems do suffer certain drawbacks.

Namely, these systems can be relatively complex, can involve the use of numerous parts, and can be relatively heavy.

Moreover, the flight control surface actuation systems that use individually driven flap and slat actuators typically rely on numerous controllers, such as one per actuator or flight control surface, which can further increase complexity and weight.

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